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1

Gibson, Lorna J. Cellular solids: Structure & properties. Oxford [Oxfordshire]: Pergamon Press, 1988.

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2

F, Ashby M., ed. Cellular solids: Structure and properties. 2nd ed. Cambridge: Cambridge University Press, 1997.

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3

The structure of the missionary call to the Sandwich Islands, 1790-1830: Sojourners among strangers. San Francisco: Mellen Research University Press, 1990.

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4

K, Hoffman Eric, and Langley Research Center, eds. Evaluation of the transient liquid phase (TLP) bonding process for Ti₃-Based honeycomb core sandwich structure. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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5

T, Andras Maria, Hepp Aloysius F, and United States. National Aeronautics and Space Administration., eds. Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid: Synthesis and structure of novel metal sulfur-containing complexes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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6

T, Andras Maria, Hepp Aloysius F, and United States. National Aeronautics and Space Administration., eds. Reactivity of [pi]-complexes of Ti, V, and Nb towards dithioacetic acid: Synthesis and structure of novel metal sulfur-containing complexes. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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7

Thomsen, O. T., E. Bozhevolnaya, and A. Lyckegaard, eds. Sandwich Structures 7: Advancing with Sandwich Structures and Materials. Dordrecht: Springer Netherlands, 2005. http://dx.doi.org/10.1007/1-4020-3848-8.

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8

Caprino, Giancarlo. Sandwich structures: Handbook. Padua: Il Prato, 1989.

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9

Ma, Wenguang, and Russell Elkin. Sandwich Structural Composites. Boca Raton: CRC Press, 2021. http://dx.doi.org/10.1201/9781003035374.

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10

Vautrin, A., ed. Mechanics of Sandwich Structures. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-015-9091-4.

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11

Hause, Terry John. Sandwich Structures: Theory and Responses. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-71895-4.

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12

Weichuan, Lin, Mbanefo Uy, and Langley Research Center, eds. Facesheet wrinkling in sandwich structures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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13

Öchsner, Andreas. Mechanics of Classical Sandwich Structures. Cham: Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-25106-1.

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14

Sandwich Historical Society (Sandwich, Ill.)., ed. Sandwich. Charleston, SC: Arcadia Pub., 2008.

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15

Lu, Tianjian, and Fengxian Xin. Vibro-Acoustics of Lightweight Sandwich Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-55358-5.

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16

Wray, S. Sandwich materials in energy absorbing structures. Manchester: UMIST, 1993.

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17

Chamis, C. C. Fiber composite sandwich thermostuctural behavior, computationalsimulation. [Washington, DC]: National Aeronautics and Space Administration, 1986.

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18

Sleight, David W. Buckling analysis of debonded sandwich panel under compression. Hampton, Va: Langley Research Center, 1995.

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19

Design of foam-filled structures. 2nd ed. Lancaster, Pa: Technomic Pub. Co., 1991.

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20

Abrate, Serge. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013.

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21

Abrate, Serge, Bruno Castanié, and Yapa D. S. Rajapakse, eds. Dynamic Failure of Composite and Sandwich Structures. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5329-7.

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22

Keller, Thomas. Use of fibre reinforced polymers in bridge construction. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2003. http://dx.doi.org/10.2749/sed007.

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<p>The aim of the present Structural Engineering Document, a state-of-the-art report, is to review the progress made worldwide in the use of fibre rein­forced polymers as structural components in bridges until the end of the year 2000.<p> Due to their advantageous material properties such as high specific strength, a large tolerance for frost and de-icing salts and, furthermore, short installation times with minimum traffic interference, fibre reinforced polymers have matured to become valuable alternative building materials for bridge structures. Today, fibre reinforced polymers are manufactured industrially to semi-finished products and ccimplete structural components, which can be easily and quickly installed or erected on site.<p> Examples of semi-finished products and structural components available are flexible tension elements, profiles stiff in bending and sandwich panels. As tension elements, especially for the purpose of strengthening, strips and sheets are available, as weil as reinforcing bars for concrete reinforcement and prestressing members for internal prestressing or external use. Profiles are available for beams and columns, and sandwich constructions especially for bridge decks. During the manufacture of the structural components fibre-optic sensors for continuous monitoring can be integrated in the materials. Adhesives are being used more and more for joining com­ponents.<p> Fibre reinforced polymers have been used in bridge construction since the mid-1980s, mostly for the strengthening of existing structures, and increas­ingly since the mid-1990s as pilot projects for new structures. In the case of new structures, three basic types of applications can be distinguished: concrete reinforcement, new hybrid structures in combination with traditional construction materials, and all-composite applications, in which the new materials are used exclusively.<p> This Structural Engineering Document also includes application and research recommendations with particular reference to Switzerland.<p> This book is aimed at both students and practising engineers, working in the field of fibre reinforced polymers, bridge design, construction, repair and strengthening.
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23

Somers, M. Buckling and postbuckling behavior of sandwich structures in the presence of a delamination. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1989.

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24

Carlsson, L. A., and G. A. Kardomateas. Structural and Failure Mechanics of Sandwich Composites. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-1-4020-3225-7.

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25

Lee, Sung W., ed. Advances in Thick Section Composite and Sandwich Structures. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-31065-3.

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26

Daniel, I. M., E. E. Gdoutos, and Y. D. S. Rajapakse, eds. Major Accomplishments in Composite Materials and Sandwich Structures. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3141-9.

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27

Martin, C. Wayne. A three-node C(superscript)0 element for analysis of laminated composite sandwich shells. Edwards, Calif: Ames Research Center, 1989.

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28

Tao, Zhang. Study of impact damage of Nomex honeycomb sandwich plates. Harbin, Heilongjiang Province, China: School of Aeronautics, Harbin Institute of Technology, 1989.

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29

Walker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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30

A, Meerschaut, ed. Incommensurate sandwiched layered compounds. Zürich, Switzerland: Trans Tech Publications, 1991.

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31

Gopalakrishnan, Srinivasan, and Yapa Rajapakse, eds. Blast Mitigation Strategies in Marine Composite and Sandwich Structures. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7170-6.

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32

The behavior of sandwich structures of isotropic and composite materials. Lancaster, Pa: Technomic Pub. Co., 1999.

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33

Numerical and experimental investigation of hollow sphere structures in sandwich panels. Stafa-Zuerich: Trans Tech Publications, 2008.

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34

Somers, M. Effect of delamination location on postbuckling behavior of sandwich structures. Haifa, Israel: Technion-Israel Institute of Technology, Faculty of Aerospace Engineering, 1989.

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35

Aßmus, Marcus. Structural Mechanics of Anti-Sandwiches. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-04354-4.

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36

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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37

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

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38

Jegley, Dawn C. Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels. Hampton, Va: Langley Research Center, 1992.

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39

Bitzer, Tom. Honeycomb technology: Materials, design, manufacturing, applications and testing. London: Chapman & Hall, 1997.

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40

Starlinger, Alois. Development of efficient finite shell elements for the analysis of sandwich structures under large deformations and global as well as local instabilities. Dusseldorf: VDI Verlag, 1991.

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41

International, Conference on Sandwich Constructions (1st 1989 Stockholm Sweden). Sandwich constructions 1: Proceedings of the First International Conference on Sandwich Constructions, 19-21 June 1989, Stockholm, Sweden : organised by the Department of Aeronautical Structures and Materials, the Royal Institute of Technology, Sweden. Cradley Health: Engineering Materials Advisory Services, 1989.

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42

Cheung, E. W. Buckling of composite sandwich cylinders under axial compression. Amsterdam: Elsevier Science Publishers, 1988.

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43

R, Tullos Thomas, ed. Handbook of adhesive bonded structural repair. Park Ridge, N.J., U.S.A: Noyes Publications, 1992.

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44

Cheung, Eric Waihon. Buckling of composite sandwich cylinders under axial compression. [Downsview, Ont.]: Dept. of Aerospace Science and Engineering, University of Toronto, 1988.

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45

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

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46

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

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47

R, Ambur Damodar, and Langley Research Center, eds. Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets. Hampton, Va: Langley Research Center, 1997.

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48

National Aeronautics and Space Administration (NASA) Staff. Sizing Single Cantilever Beam Specimens for Characterizing Facesheet/Core Peel Debonding in Sandwich Structure. Independently Published, 2019.

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49

National Aeronautics and Space Administration (NASA) Staff. Elevated Temperature, Residual Compressive Strength of Impact-Damaged Sandwich Structure Manufactured Out-Of-Autoclave. Independently Published, 2019.

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50

Sahlins, Marshall David. Historical Metaphors and Mythical Realities: Structure in the Early History of the Sandwich Islands Kingdom. University of Michigan Press, 2009.

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